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Movable leading edge flaps for aircraft aerofoil wings and wings with such movable leading edge flaps
Movable leading edge flaps for aircraft aerofoil wings and wings with such movable leading edge flaps
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机译:用于飞机机翼机翼的可移动前缘襟翼以及具有这种可移动前缘襟翼的机翼
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摘要
The invention relates to a leading edge mobile flap (16) for a main wing of an aircraft, this flap including an aerodynamic skin (18) that has a bird impact-sensitive frontal area (24), and a rear skin (28) integral with the aerodynamic skin (18), the flap also comprising a plurality of ribs (34) spaced out along a leading edge longitudinal direction (X). According to the invention, the flap additionally includes, between two directly consecutive ribs, a single rigid bird trajectory-deflecting wall (42) anchored to the skins (18, 28). Furthermore, in a cross-section taken along any plane orthogonal to the direction (X), the wall (42) forms with a geometric chord (26) of the flap an angle (1) with a value of less than 45°.
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